• DocumentCode
    841673
  • Title

    On the feasibility of real-time prediction of aircraft carrier motion at sea

  • Author

    Sidar, Menahem M. ; Doolin, Brian F.

  • Author_Institution
    NASA, Moffett Field, CA, USA
  • Volume
    28
  • Issue
    3
  • fYear
    1983
  • fDate
    3/1/1983 12:00:00 AM
  • Firstpage
    350
  • Lastpage
    356
  • Abstract
    Landing aircraft on board carriers is a most delicate phase of flight operations at sea. The ability to predict the aircraft carrier´s motion over an interval of several seconds within reasonable error bounds may allow an improvement in touchdown dispersion and reduce the value of the ramp clearance due to a smoother aircraft trajectory. Also, improved information to the landing signal officer should decrease the number of waveoffs substantially. This paper indicates and shows quantitatively that, based upon the power density spectrum data for pitch and heave measured for various ships and sea conditions, the motion can be predicted well for up to 15 s. Moreover, the zero crossover times for both pitch and heave motions can be predicted with impressive accuracy. The predictor was designed on the basis of Kalman´s optimum filtering theory (the discrete time case), being compatible with real-time digital computer operation.
  • Keywords
    Aircraft landing guidance; Kalman filtering, linear systems; Marine-vehicle control; Motion measurements; Prediction methods; Accuracy; Aircraft; Density measurement; Filtering theory; Kalman filters; Marine vehicles; Motion measurement; Power measurement; Sea measurements; Trajectory;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9286
  • Type

    jour

  • DOI
    10.1109/TAC.1983.1103227
  • Filename
    1103227